What was found
AD 2020-17-03 / A.A WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT . FLIGHT DECK, WINDSHIELD FRAMING, L/H R/H CONTINUITY FITTING CRACKED. CONTACT LIAISON ENGINEERING FOR FURTHER DISPOSITION. PERFORMED NOSE FWD FUSELAGE I FRONT WINDSHIELD FRAME AND L/H R/H CONTINUITY FITTINGS REPLACEMENT I/A/W DELTA ER/A NO 635072-14AD SECTION I REV: ORIGINAL DATED 24-JUL-26. NOTE: REPAIR APPROVAL IS LIMITED TO 60.000 TOTAL FLIGHT CYCLES (ESG). ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. SECTION DTE AND LOG PAGE #1717978 ARE ESTABLISHED TO ENSURE THAT AIRBUS IS CONTACTED PRIOR TO THIS THRESHOLD FOR INSPECTION METHOD AND REPETITEVE INSPECTION LIMITS. CLOSING ACCESS AND TESTING WAS PERFORMED AS PER ER/A #635408-14 SECTION I REVISION ORIGINAL DATED 05-AUG-26. ASSOCIATED ER/A 00-635072 ADDED FOR AC 3252. (LP: 1741900, AIRCRAFT WAS GROUNDED)